Antiaircraft gun



June 27, 1944. J. A. VEIT ANTI-AIRCRAFT GUN Filed Dec. 10, 1941 9 Sheets-Sheet 1 t]. (E e 2'13,

INVENTOR.

A TTOR/VZ Y June 27,1944. J A, VE|T 2,352,577

ANTI-AIRCRAFT GUN Filed Dec. 10, 1941 9 Sheets-Sheet 2 Q/TJZ 5/62/1 INVENTOR.

A rromvsy June 27, 1944. A v5" 2,352,577

ANTI AIRCRAFT GUN Filed Dec. 10, 1941 9 Sheets-Sheet 5 mm. n y g /7 7 /9-%' is M i *z -J-q 0 7/ l8 w \E /z 2,3

June 27, 1944. J. A. VElT ANTI-AIRCRAFT GUN Filed Dec. 10, 1941 9 Sheets-Sheet 4 Jfl. IZZ Z IN VEN TOR.

A rra/mz Y June 27, 1944. J v n- 2,352,577

ANTI-AIRCRAFT GUN Filed Dec. 10, 1941 9 SheetsSheet 5 as 8/ 72 87 51?; Z7

I N VEN TOR.

A T'T'OR/VE Y J. A. VEIIT 9 Sheets-Sheet 7 ANTI-AIRCRAFT GUN Filed Dec. 10, 1941 June 27, 1944;

June 27, 1944. J. A. VEIT ANTI-AIRCRAFT GUN Filed Dec. 10, 1941 9 Sheets-Sheet 8 RNMWN EN WN m m I I i 15:

June 27, 1944. J. A; VEIT 2,352,577

ANTI-AIRCRAFT GUN Filed Dec. 10, 1941 9 Sheets-Sheet 9 76 II "W 6 79 (Zfl. Vit INVENTOR.

BY I,

ATTO/F/VEY Patented June 27, 1944 UNETE STATES P This invention aims to provide novel means for pointing a piece of artillery at an airplane in flight, the construction being such that the piece may be; made to follow the lane, regardless of the flight of the plane, considered vertically or horizontally.

The invention aims to supply novel means for mounting the artillery piece and controlling its movements at the will of operators.

It is within the province of the disclosure to improve generally and to enhance the utility of devices of that type to which the present invention appertains.

With the above and other objects in view, which will appear as the description proceeds, the invention resides in the combination and arrangement of parts and in the details of construction hereinafter described and claimed, it being understood that changes in the precise embodiment of the invention herein disclosed, may be made within the scope of what is claimed, without departing from the spirit of the invention.

In the accompanying drawings: 7

Fig. 1 shows in side elevation, a device constructed in accordance with the invention;

Fig. 2 is a section on the line 2-2 of Fig. 1, most parts appearing in elevation;

Fig. 3 is a section on the line 3-3 of Fig. 2;

Fig. 4 is a section on the line4-fl of Fig. 3;

Fig. 5 is a top plan;

Fig. 6 is an elevation showing one of the telescope tubes and the trigger mechanism that is carried thereby;

Fig. 7 is an elevation illustrating the telescopes and portions of the structure which carries them;

Fig. 8 is a top plan of the telescopes and attendant parts, portions being broken away;

Fig. 9 is an elevation showing a casing which is located adjacent to the telescopes;

Fig. 10 is a horizontal section of the structure shown in Fig. 9;

Fig. 11 is a top plan, with parts in section. showing portions of a gear shift mechanism that is employed;

Fig. 12 is a diagrammatic elevation showing certain of the gear members;

.Fig. 12A is a diagrammatic elevation disclosing further details of the structure depicted in Fig. 11; p

' Fig. 13 is a sectional view showing the pawl and ratchet mechanism employed in the structure delineated in Fig. 11;

Fig. 14 is an elevation showing a portion of the structure which has to do with the electrical features of the device, hereinafter set forth;

Fig. 15 is a. section on the line l5-I5 of Fig. 14;

Fig. 16 is an elevation showing the rotor and attendant parts;

Fig. 17 is a section on the line ll-ll of Fig. 16;

Fig. 18 is a circuit diagram;

Fig. 19 is a diagrammatic view employed in explaining the operation of one of the component mechanisms.

In carrying out the invention, there is provided a support S (Fig. 1), including a base i, in which the lower end of a vertical standard 2 is mounted to rotate, the standard being provided at its upper end with a fork 3, (Figs. 2 and 4). The standard 2 likewise may be referred to as a support, since practically all working parts of the device are carried by it. A gear wheel 4 (Fig. 1) is secured to the lower portion of the standard 2 and is housed within the base I, the gear wheel meshing with a pinion 5, secured to a vertical shaft 6, which passes into the casing of a speed reduction mechanism 7, the casing being mounted on the standard 2. The speed reduction mechanism 7 is coupled to the shaft I00 of an electrical motor 8, carried by the standard 2. The speed reduction mechanism 1 cannot be de scribed conveniently at this stage of the specification. For the purposes of the present discussion it is sufficient to state that the motor 8 is a reversing motor, capable of imparting direct or reverse rotationto the standard 2.

A U-shaped frame 9 (Figs. 2 and 4) is disposed between the arms of the fork 3, the side members of the frame merging at their upper ends into gear segments in (Fig. 3). One side member of the frame 8 is mounted (Fig. 4) to swing on a pivot element II in one arm of the fork 3, the opposite side member of the frame heing'mounted to swing with the rotation of a shaft l2, mounted to rock in the adjacent arm of the fork, the shaft forming part of a speed reduction mechanism within a casing M (Fig. 2) The speed reduction mechanism is coupled to the shaft Hll of an electrical motor l5 (Fig. 1). A bracket Hi on one arm of the fork 3 supports the motor l5 and the speed reduction mechanism in the casing I4. The speed reduction mechanism in the casing I 4 duplicates that in the casing 1 and is reserved for further discussion. The motor I5 is a reversing motor and imparts direct and reverse rotation to the shaft. l2.

A horizontal shaft l1 (Figs. 2 and 4) is disposed between the arms of the fork 3. a ring l8 being interposed in the shaft. The shaft IT is provided at its ends with gear segments l9, which mesh with the gear segments H! on the frame 9. The

. jectiles. of the present invention. It is intended that the observers at the' telescopes 46, 41 and 48 shall shaft includes detachable end sections 20, mounted to rotate in the side arms of the fork 3.

' spective telescopes, when the standard 2 of Fig.1,

A sleeve 2| (Figs. 1, 3 and 4) extends through the ring l3, and is circumferentially grooved, as

at 22, to receive the ring, the sleeve thus being mounted to rotate in the ring. The shaft I1 and associated movable parts may be called a carrier.

motor 25. a The motor 25 and the speed reduction mechanism 25 are carried by a bridge 21, which isfixed to the segments I3 along the surfaces 21a of Fig.4.

and parts carried by it, are rotated. Chairs, slings" or couches for that purposeas used in observatories are known in the art, and are beyond the purview of the present disclosure. The train of parts which operates to produce a verticalcomponent in the pointing ofthebarrel 3|, includes the motor. l5,of Fig. 2, the speed reduction gearing in the casing M, the 'intermeshing segmentsflll and 13, the shaft 20 -41 of Fig. 4, the ring I8, the sleeve 2|, the bearings 33. and the trunnions 32. Note,-however,.that th barrel 3| does not have vertical swinging movement by way of thetrunnions 32 and 'the In order to prevent the sleeve 2| from sagging I downwardly; in the direction of the arrow A in Fig. ,3, with the shaft |'I20 of Fig. 4 as an axis of sagging movement, the bridge 21 has depending arms 28 (Fig. 2), located on opposite sides of the sleeve, and provided with beads 29, which are received in acircumferential groove 30 (Figs.

2 and 3), fashioned in the sleeve and located to the rear of the groove 22 that receives the ring l8. f

A gun barrel 3| extends through the sleeve 2| and is provided intermediat its ends with trunnions 32 (Figs. '2 and 4), mounted to rock in bearings 33, secured to the inner surface of the sleeve 2|. The barrel 3| has any desired number of lines of bores, designated'at 34, 35 and 36,

respectively, the line 35 being the intermediate line. The lines 34, 35 and 36' are disposed iniparallelism, longitudinally of the axis of the bar- ,rel 3|. All of th bores 34, 35 and36 are located in agroup of narrow cross-sectional area con-' sidered relatively to the cross-section of the barrel, the group being of unequal transverse dimensions, the longer transverse dimension. of the group extending from a. point near the longitudinal axis of the barrel to a'point closely adjacent ,tothe perimeter of the barrel.

A yoke 31 is-secured to the barrel 3| (Fig.3), in advance of the standard 2, an upwardly extended rack bar 38 being pivotally connected at 33 to the yoke. A pinion 40 meshes with the rack bar 38, and issecured to the'shaft 4| of'a.

speed reduction mechanism 43 coupled to a reversing electric motor 42. The motor and the speed reduction mechanism 43 aremounted on a bracket 44, carried by the gear wheel 23 at the ,7

to participate. in the movements of the barrel.

Referring to Fig, 2. the telescope 48 has cross wires 52 are disposed in an eye piece 53 (Fig. 8),

which is rotatable with respect to the body of the telescope 41, the eye piece having a hand wheel 54 (Fig. '7) by which it may be rotated. 1 An observer at the telescope 45 may focus all three of the telescopes by any simple mechanism, such as that shown at 55 in Fig. ,8. The telescope 46 carries a'pistol grip and trigger 56, (Fig. 6)

by the shaft 20-41.

bearings 33 in this step of the operation, independently of the sleeve 2|, because therack bar 38 of Fig. 3 is engaged with the pinion 40. The axis of vertical tilting movement is represented The train of parts which produce a hor izontal component in the pointingof the barrel 3|.ln-

- cludesthe motor 8 of Fig. 1, the shaft 5, the speed reduction gearing in the casing I, the pinion 5, the gear wheel 4. the rotatable standard}, the fork 3. and those parts shown hi 2 which connect the barrel 3| to the fork, for; horizontal movemcntl Since the pointing of the barrel 3| has both vertical and horizontal components, the piece may be aimed at an airplane, regardless of the position of 'the plane as to elevation or as to azimuth. s

A rotation of the barrel 3| is required inorder that projectiles fired. from the intermediate line 35 of bores in Fig. ,4 shall coincide with the line of flight of the plane,when the line of advance is horizontal, upwardly, downwardly, or at an angle of less than ninety degrees with respect to the horizontal. The rotation of the-barrel 3| about its longitudinal axis serves'to align the longer transverse dimension of the group of bores 34, 35 and 38, with the pathof flight of the aircraft which is being attacked. The projectiles discharged from the lines 34 and 36 in Fig. 4

. promote the probability of 'destruction,'if the aimng'is n'ot so'accurate. that the projectiles discharged from the line 35, alone, can be relied,

upon. v V s By means of the hand wheel '54 'of Fig. '7, the

d observer at thetelescope 41. can rotate the eye piece 53, and with it, the parallel wires 52, the image of the airplane'being kept between those wires,.regardlessofwhetherthe line of flight is upwardly at an angle, downwardly at an angle,

60 wires 50, the telescope 45 has cross wires 5|. and the telescope 41 has parallel wires 52. The cross horizontal, 'or vertical. A mechanism to badescribed hereinafter is provided whereby when the eye piece 53 is rotated, the barrel 3|. will be rotated, thus'keeping the line of bores "35 (Fig. 4)

between the parallel wires 52. Q

The train of parts .hereinbefore described which produces a rotation of the barrel 3| on its axis, includes the motor 25of Fig; 1, the speed change mechanism 26, the pinion 24, the gear wheel '23 and the sleeve 2|. The sleeve 2| is mounted to rotate in the ring |8 of Fig. ,4, and the ring is carried by the shaft ||---2|l which-is mountdin the fork 3. v V

Assume, byway of illustration,- that the plane is flying'upwardly and to the right in Fig. 4, the

for causing the gun barrel 3| to discharge pro- The firing mechanism forms no part maintain'fixed positions withjregard to the rebarrel 3| having been rotated on its longitudinal axis (Fig' 3) until the intermediatelline of bores 35 in Fig. 4 is parallel to'fland coincident with the line of fiight.- It is also desirable to tilt the barrel 3| on the trunnions 32 and the bearings 33 in order that the barrel may be aimed with alead on the advancing plane. The lead is in train if being rotated by a hand wheel 15.

the plane to be attacked is in horizontal flight, but the lead will hav a vertical component if the plane ismoving along a path other than horizontal. The means for giving th barrel 2. lead, as aforesaid, includes the motor 2 of Fig. 3,

the shaft ll, the speed change mechanism 43,

the pinion 40, the rack bar 38 and the yoke 31. The observer at the telescope MS has under his control a means whereby the horizontal and vertical components in the pointing of that telescope are determined, and whereby the lead" is governed. The observer at the telescope 41 keeps that telescope so pointed that the airplane appears between the parallel wires 52 of Fig. 2.

i A means next to be described is provided whereby the barrel 3| moves in consonance with the telescopes l6, l1 and 4B. The observer at the tele- "scope l8 simply is in general charge, and issues orders to the observer at the telescope it, especially as to pressing the trigger 55 and firing the gun; and to the observer at the telescope 61, if his eflorts call for supervision.

As to the means whereby the barrel 3! is caused to move in consonance with the movements of .the telescopes 4B, 41 and 48, attention is directed to Figs. 9, l and 18. A casing 51 is mounted underneath the telescope 46. and in it is journaled a shaft 58, carrying a finger 59, adapted to cooperate with a dial 60 on the casing, and calibrated in volts, the shaft being rotated by a hand wheel 6|. In Fig. 18 there are shown electric mains 62, the primary coil of a transformer appearing at 63, and the secondary at 64. Any

. desired number of leads 65 are taken off the secvoltage delivered to the conductor ll.

If the plane is flying horizontally, the vertical component is zero, and the motor l must be idle,

the motor 8 operating at a speed determined by the horizontal speed of the plane. If the plane is flying vertically, the horizontal component is zero, and the motor 8 must be idle, the motor 85 operating at a speed determined by the vertical speed of the plane. If the plane is flying otherwise than horizontally, the motors, t and It must operate at times at the same speed, for example,

,when the line of flight is at 45 degrees, 135 degrees, 225 degrees or 315 degrees.

The motors 8 and I5 must operate at different speeds if the line of flight is otherwise than as last-above stated, or is changing constantly. The speed at which the motors t and i5 operate depends on the voltage delivered to them, respectively. Th current traversing the'conductcr ll ultimately reaches the motors ii and ill. but it must be regulated as to each of them. A means to that end is shown in the upper right hand corner of Fig. 18, and its construction will next be set forth.

Reverting to Figs. 9, l0 and 18. a shaft it is mounted to rotate in the casing 51' and carries a finger 13. adapted to cooperate with a dial it on the casing, and calibrated in degrees, the shaft The conductor H is connected to one end of a resistance It, and is connected by a conductor ll to the opposite end of a resistance it.

Any desired and a corresponding number of leads 3| run from the resistance 78 to a circle of contact points E2 on the casing. The contact points B0 are adapted to be engaged by a finger 83, on a collar it which is carriedby the shaft 12, and the contact points 92 are adapted to be engaged by a finger til on a collar 86 carried by the shaft. The casing El supports a brush 81 making contact with the collar 84, and a brush 88 making contact with the collar 86. A conductor 89 is joined to the brush 81, a conductor 90 being Joined to the brush dd.

The conductor 89 furnishes current to the motor a of Fig. 1, which produces the lateral com- .ponent, and the conductor til furnishes current to the motor Iii of Fig. 2, which produces the vertical component. The device shown in Figs. 9 and 10. and in the upper, right hand corner of Fig. 18, affords a means whereby the voltage supplied to the motors t and ill may be altered at the will of an operator. Owing to the manner in which the leads "I9 and iii are taken off the resistances Hi and 18, respectively, together tvitl'r th manner in which the lingers t5 and cc operate with the contact points iii. and the voltage supplied to the motor it rises as the voltage supplied to the motor 5 falls, and vice versa. The motors t3 and iii operate at governed speeds, under the control of an operator at the hand wheel of Figs. 2 and i0, and the horizontal and vertical components in the pointing oi the gun 3| are regulated as occasion may require.

Noting diagrammatic Fig. 19, it will he understood that the gun barrel iii, responding to the motors B and I5. must b capable of being pointed anywhere around the circumference there repre sented, and it must be capable oi moving in each of the two directions indicated by the arrows. The motors 8 and i5 are reversing motors,' and it is clear that they must be reversed at the points A. B, C, and D. nothing more intricate than the relative values of the sine and cosine of any angle being involved. The means for reversing the motors ii and I5 will next be described.

The construction of the speed reduction. gearing for the motor I5 of Fig. 2. and located in the casing it, is shown in Figs. 11 to 13. "3 Hit of the motor it enters the casing i plied with a worm 9t, meshing with ti on a shaft 92, the shaft til being provided with a worm l90. meshing with a worm wheel on a shaft 9 the shafts being supported for rotation on the casing. The shaft carries pinion 96, meshing with a gear wheel 9'? on. the shaft 62 of the speed reduction gearing. The con struction is such that when the motor reverses its shaft till, the shaft it will be reversed also. a vertical component being contributed to the pointing of the gun barrel fl i.

A sleeve Eltis rotatable on the shaft iii carries a gear wheel til, which has a ratchet on one side. The gear wheel meshes with a gear wheel tilt rotatable on a shaft it t. carried by brackets "35 on thecasing i i. The gear wheel tilt is integral with a gear wheel tilt, which onacts with a gear wheel llll fixed to the shaft lit. The gear wheel lt'l carries a spring-pressed pawl Hi8. adapted to cooperate with the ratchet it? of the gear wheel 99. Solenoid soils 9 a d E513 a e mounted at Ill in the casing Hi and an armature H2 is responsive to them. The armature ife has a lateral fork Ht received between shoulde s. on a shaft H5 having rotation and straight line reciprocation in depending parts, of the brackets r versed.

I35. the-conductor I31.the conductor I38, and

I05. A pinion H6 is secured to the shaft 5 and is adapted to be movedinto and out of mesh with the gear Wheels I06 and I01. I I

The shaft -I2 may be driven directly or in reverse, in consonance with the shaft IOI of the ..motor I5, and the shaft 6 may be driven directlyor in reverse, in consonance with the shaft I I of the motor 8..reyersals taking place, as to the is introduced into the aimingof the gun 3I, occurs 7 at the points Band D of Fig; ;19i The casing 1 of Fig. 2 containsa mechanismv difl'eringfrom vthe mechanism enclosed in the casing I4 only in that, as .shown'in Fig. 18,.the track members I33 and I40 are divided horizontally, as at I 4| ,to bring about a reversal at the points D and B of Fig-19,

shaft 6, atithe points D and B of Fig. 19, and-as to theshaft I2, at the points A and C, as more fully described hereinafter. By moving th pinion H6 into and out of mesh with the gear wheels I06 and I01, when the reversals take place at A, B,"C and D. the sleeve. 98 maybe kept running in one direction. even though the directionoffrotation of the shaft I2 has been reversed. due to a reversal of'the motor I and its shaft IOI. The reason whyv the sleeve 98 must maintain a continuous direction of rotation will be made manifest hereinafter.

Noting Fi in conjunction with Fig. 18, the sleeve 98 has insulated hubs H1 and H8 provided. respectively, with arms H9 and I20. The arm I traverses a circular outer track on the casing I4. and the arm II8 traverses a circular,

inner track on the casing The outer track (Fig.'

18) is divided vertically, to form semi-circular members I2I and I22. The inner track is similarly divided, to form semi-circular members I23 and I24. The conductor 90 is joined electrically. as at I25, to the trackmemb'er I24, and at I26 to the track member I2I.

The casing. I4 (Fig. 15) supports a brush I21 which engages the hub H8. and a brush I28 which engages the'hub I I1. A conductor I29 con- The electrical equipment, marked as, a whole by the numeral I42, has. no distinguishing characteristics which call for lengthy description, in, view of what has been explained hereinbefore, in connection with themotor I5. The motor 8, however,

receivescurrent from the conductor 7 rather than from the conductor 90;

; Suppose that the direction of rotation ofthe shaft IOI of the motor I5 were reversed, and that the arms IIS and I20, ofv Figs. 18 and 15 were ;-mount'ed on the shaft I2, instead of onthe sleeye v98. In that case, the arms IIS and I20 'would simply oscillate back and. forth through a small are at one of the places where the track members I2I-I23 and 122-424 are separated terminally, and there would be no more than a continuous and flutteringreversal 0f the-mot0r I5. It is necessary that the sleeve rotate in one direction, even though the direction of irotationfof the motor shaft is reversed. Z

A conductor I43 joins the, track member I22 to the intake end of the winding of the solioid magnet I I0,and a conductor I44 joins thetrack member I23to theintake end of the winding of the sol'enoid magnet I09, The outlet ends of the windings of the magnets I08 and H0 are joined heats the brush I21 with one side of the motor I5. and a conductor I30 connects the brush I28 with the oppositeside of the motor I5. Aconductor I32 connects, the track member I22 with the track member I23, and from'the track member I23 there leads a conductor I34. in which the field I35 of the motor I5 is interposed. The field by a conductor I45, and fromthe conductor I45 a conductor I46 leads to the conductor I31, and current flows by way of the conductor I38 to the secondary 64 of the transformer. .Referringto l35 of the motor I5 is joined by a conductor I31 to a conductor I38 which is connected to the secondary 64 of the transformer.

Disregard for the moment the functioning of the mechanism shown in Figs. 11 to 13. and assume that the arms' lll-l and I20 are in the positions shown in Fig. 18. Then there is established a circuit which includes the conductor 90. the conductor I25. the track member I24. the arm I IBhthe hub II1, the brush I28. the conductonI-"l, the

motor I5. the conductor I29. the brush 121. the hub II8. the arm I20. the track member. I22. the conductor I32, the conductor I34. the field (I35. the conductor I31. the conductor I38. and the sec- 7 ondary 64 of the transformer.

Suppose that the arm I20 cngageslhe track member I2I. the arm II9 enga ing the track member I23. Then there is established a circuit.

comprising the conductor 90. the conductor I25 the conductor I26. the track member I2I. thearm' I20, the hub us. the brush I21,.the conductor I29, the motor I5. the conductor-I30. th brush I28. the hub II1. the arm II8. the trackmember I23 and the conductor I34. and the motor I5 is The circuit is completed by the field the secondary 64 of the transfo'rmen.

The r versal ofthe motor I5.'said motor being the instrumentalit whereby the vertical. com- DOnFl'It is introduced into the a min of the un 3!. occurs at the points A and C of Fi 19. The

reversal of the motor 8. said motor being the in- Y strumentality whereby the horizontal component Figs. 11 to 13, rotationmay be imparted to the sleeve 98. by the pawl I08 of the-gear .wheel I01 andthe ratchet I02 of the gear Wheel 99, the pinion I I 6 being out of mesh with the gear wheel I06'and the gear wheel. I01. By the energization of the appropriate magnet I09 or I I0, the pinion H6 is introduced between the gear wheels 10! and I01. The sleeve 98 then continues torotate in the same direction, even though the direction .of rotation of the motor shaftv IOI has been reversed. the pawl I08 clicking Over the ratchet I02. 1 t

Referring to Figs. 8, 9, 10, 16, 17 and 18, the shaft 58 and parts next to be described govern the operation o'f the motor 42 of Fig. 1,-which functions to give a lead to the gun barrel 3I.T

'From. any portion of the secondary of'the transformer, there leads a conductor I5I.which is joined to a ponducton I53. connected to a brush I50 (Fig. 10)" on the casing 51. The brush I50 makes contact with an insulated collar I54 on the shaft 58. The collar I54:has a finger I55. adapted to engage any of a plurality of contacts I56 on' the casing 51. Of these contacts. there maybe any desired number, a conductor I51 being joined to each contact. j

Noting Figs. 16 and 17, the conductors I51 are joined to electro-magnets I58. fixed in a circle in. the casing of. the speedreduction mechanism 43, the electro-magnets forming part of a magnetic switch. The e'lectro-magnets I58. are severally joined by conductors I59 to a conductor I60. joined to a conductor I61, which is connectedto the conductor I38. I I

The circuit foreachele'ctro-magnet I58 includes the conductor I5I. the conductor I53, the brush I50 Fig. 10 the hub I54. the finger I55. the contact I56, the conductor I51. the magnet as of Fig. rs,

I58, the conductor I59, the conductor I60, the conductor I6I, the conductor I38, and the secondary 64 of the transformer.

Considering Figs. 16 and 17, a switch mechanism is provided and includes a rotor I62 having a hub I63 rotatable on the shaft 4| (Fig. 1) of the speed reduction gearing 43 that is assembled with the motor 42. The rotor I62 has a periph-' eral armature I64, responsive to the particular electro-magnet I58 that happens to be energized. The rotor I62 has an outer track, made up of semicircular members I65 and I66; and an inner track, made up of semicircular members I61 and I68. The ends of the track members I65 and I61 A sleeve I12, (Figure 17) is secured to the hub I63 of the rotor I62 and is circumscribed by an insulated sleeve I13. The sleeve I13is connected electrically to the track member I66, as shown at I14, the sleeve I12 being connected electrically to the track member I 65, as shown at I15. Fixed brushes are carried by the casing 43, the brush I18 cooperating with the sleeve I12, and the brush I11 cooperating with the sleeve I13. A conductor I18 is connected to the brush I11 and is joined to the conductor 1|. A sleeve I19 is secured to but insulated from the shaft 4|. A sleeve I89 is secured to but insulated from the sleeve I19.

The sleeve I88 has an arm I8I, adapted to engage electrically with the track members I88 and I66, one at a time. The sleeve I19 has an arm I82, adapted to engage the track members I61 and I68, one at a time. The casing 43 carries a brush I83, engaging the sleeve I19, and a brush I84 engaging the sleeve I86. A conductor I85 joins the brush I84 to one side of the motor 42. A conductor I86 extends from the opposite side of the motor 42 and is joined to the brush I83. A conductor I81 joins the brush I16 to the field I88 of the motor 42. A conductor I89 joins the field I88 to the common return I38.

Suppose that, by an appropriate rotation of the hand wheel 6| and the shaft 58 of Fig. 10, the appropriate electrode magnet I58 is energized, through the magnet circuit herelnbefore traced out. The selected electrode magnet I59 attracts the armature I64 on the rotor I62, and the rotor makes a partial rotation on the shaft 4|, until the armature I64 reaches the selected electrode magnet I58. As soon as the rotor I62 starts to rotate, counterclockwise in Fig. 18, the finger I 8| comes into contact with the track member I65, and the finger I82 comes into contact with the track member I68.

Then there is established a circuit comprising the conductor 1|, the conductor I18, the brush I11, the sleeve I13, the connection I14, the track member I66, the finger I8I, the sleeve I89, the brush I84, the conductor I85, the motor 42, the conductor I86, the brush I83, the sleeve I19, the finger I82, the track member I68, the conductor I1I, the track member I65, the connection brush I15, the sleeve I12, the conductor I81, the field |88, the conductor I89, and the return conductor I38. Under such circumstances, the motor 42 has direct rotation.

By an appropriate rotation of the hand wheel 6| and the shaft 58 of Fig lO, the rotor I62 15 caused to rotate clockwise in Fig. 18. The finger I8I is on the track member I65, and the finger I82 is on the track member I61. Then there is established a circuit comprising the conductor 1|, the conductor I18, the brush I11, the sleeve I13, the connection I14, the track member I66, the conductor I10, the track member I61, the finger I82, the sleeve I19, the brush 183, the conductor I86, the motor 42, the conductor I85, the brush I84, the sleeve I88, the finger I8I, the track I65, the conductor I15, the sleeve I12, the brush I16, the conductor I81, the field I88, the conductors I89 and I38. The motor 42 then is operating in reverse.

From the foregoing it will be noted that the operator has under his control, the means whereby the motor 42 of Fig, 1 may be operated directly of in reverse to impart swinging movement to the gun 3|, and to give the gun a lead on the flying airplane.

From what has been stated up to this point, it appears that the observer at the telescope 46 has several duties to perform. He focuses all of the -telescopes 46, 41 and 48. He controls the motors 8 and I5, which produce the horizontal and yer tical components in the pointing of the gun barrel, he controls the motor 42 which gives the lead and he presses the trigger 56 of Fig. 6, to fire the gun. Should these duties prove too onerous, the trigger 56 might be placed on one of the other telescopes, for example the telescope 48. As to the focussing, the structure shown at 55 is such that the focussing might be done elsewhere than at the telescope 46. It is the duty of the observer at the telescope 41 to rotate the eye piece 53 of Fig. 8, by means of the hand wheel 54 of Fig. 7, to keep the wires 52 parallel to the line of flight of the plane, with the image of the plane between them, the gun barrel 3| being rotated axially, so that the line 35 of bores in Fig. 4 follows the line of flight of the plane, the particular bore of the line 35 that is in the axis of the barrel being directly on the airplane. The function referred to results from the operation of the motor 25, as hereinafter set forth. The means for accomplishing that result will now be set forth in few words, since the component mechanisms are substantial duplicates of others hereinbefore described.

Referring to Fig. 18, there is provided at I98 a magnetic switch like that shown in Figs. 16 and 17, and contained within the gear casing 26 of Fig. 3. The intake conductor for the motor 25 is shown at |9I and is connected to the con ductor 1|. As to the controlling connection between the eye piece 53 of the sighting device 41 and the mechanism for rotating the barrel 3|, the rotatable eye piece part 53 of Fig. 8 carries a finger I92 traversing contacts I93 mounted in a ring I94 in a casing I95 secured to the fixed portion of the telescope 41. Conductors I96 lead to the electro-magnets I91 of the switch .190, thoseelectro-magnets corresponding to the electro-magnets I58 of Figs. l6, l7 and 18. The conductor I5I leads to a brush I98, making contact with a ring I99, carrying the finger I92. By rotating the eye piece 53 of the telescope 41 (Fig. 8), corresponding movement by the motor 25 is brought about. To trace out the circuits would be merely a restatement of the operation of the magnet switch already described, and a retracing of the circuits seems unnecessary By way of rsum, by rotating the hand wheels 6| and 15 of Figs. 2 and 10, the operator at the telescope 46 of Fig. 8 regulates the voltage supplied to themotors 8 and I and apportionsthev current between them, the motors operating at various speeds relatively to eachother, and horizontal and vertical components being determined'in the pointing of the gun barrel 3|. He

the group with the path a flight of the aircraft,

also determines the guniead, since the motor 42 The operator at the tele-' and a controlling connection operatively connected to the rotatable part of the sighting device and to said. mechanism.

4. In a device for pointing a gun atan airplane inflight, a support, means for mounting the support for rotation about a substantially vertical axis, a gun barrel having bores, all of which are located in. a group of narrow cross-sectional area considered relatively to the cross-section, of the barrel, the group'being of unequal transverse out utility as the angle departs from ninety degrees.

Having thus described the invention, what is claimed is: i

1. Ina device for pointing a gun at an aircraft in flight, a 'gun barrel having bores, all of which are located in agroup of narrow cross-sectional area'considered relatively to the cross-section of the barrel, the group being of unequal transverse dimensions, the longer transverse dimension of the group extending from a point near the longitudinal axis of the barrel to a point closely adjacent to the perimeter of the barrel, means for mounting the barrel for vertical swinging movement and for horizontal swinging movement, each at the will of an operator, and for rotation on its longitudinalaxis, to align the longer transverse dimension of, the group with the path of flight of the aircraft, and mechanism under the control of an operator for rotating the barrel on its longitudinal axis.

2. In a device for pointing a gun at an aircraft in flight, a support, means for mounting the support for rotation about a substantially vertical axis, a gun barrel having bores, all of which are located in a group of narrow cross-sectional area considered relatively to the cross-section of the barrel, the group being of unequal transverse dimensions, the longer'transverse dimension of the group extending from a point near the longitudinal axis of the barrel to a point closely adjacent to the perimeter of the barrel, and means tion on its longitudinal axis, to align the longer transverse axis of the group with thepath of flight of the aircraft, and for swinging movement along the line of flight of the aircraft, to afford a lead for each position to which the barrel may have been rotated on its longitudinal axis.

3. In a device for pointing a gun at an aircraft in flight, a gun barrel having bores, all of which are located in a group of narrow cross-sectional area considered relatively to the cross-section of the barrel, the group being of unequal transverse dimensions, the longer transverse dimension. of the group extending from a point near the longitudinal axis of the barrel to a point closely adjacent to the perimeter of the barrel, means for mounting the barrel for horizontal and vertical swinging movements and for rotation onits longitudinal axis, a sighting device connected to the barrel, to participate in the movements of the barrel, and including a rotatable part, mechanism for rotating the barrel on its longitudinal axis, to align the longer transverse dimension of dimensions, the longer transverse dimension of the group extending from a point near the longitudinal axis of the barrel to a. point closely adjacent to the perimeter of the barrel, means for mounting the barrel on the support for substantially vertical swinging movement, for rotation on its longitudinahaxis, to align the longer transverse dimension of the group with the path of flight of the aircraft, and for. swinging movement along the line of flight or the aircraft, to afford a lead for each position to which the barrel may have been rotated on its longitudlnalaxis; a, sighting device operatively connected to the barrel, to participate in the movements of the. barrel, mechanism for imparting rotation to the's'upport, mechanism for imparting said substantially vertical swinging movement to the barrel, and a control for each of said mechanisms, the. controls I relatively to the cross-section of the barrel, thebeing located conveniently with respect to an observer atv the sighting device.

5., A device for pointing a gun at an aircraft in flight, constructed as set forth inclaim 4, in combination with a second sighting device operativelyconnected to the barrel, to participate in the movements of the barrel, the second sighting device including a rotatable part, mechanism for rotating the barrel on its longitudinal axis, and a controlling connection operatively connected to the last-specified mechanism and to the rotatable part ofthe second-sighting, device.

6. .In a device for pointing a gun at an aircraft inflight, a'support, means for mountingthe sup+ port'for rotation about a substantially vertical axis, a carrier, a barrel projecting from the car'- rier and having bores, all of whichare located in a group of narrow cross-sectional area considered group being of unequal transverse dimensions, the longer transverse dimension of the group extending from a point near the longitudinal axis of the barrel to a point closely adjacent to. the perimeter of the barrel, means for pivoting the carrier to the support, to permit vertical swinging movement of the barrel, a member mounted on the carrier for rotation in a plane transverse to the longitudinal axis of the barrel, to alignthe longer transverse dimension of the group with the path of flight of the aircraft, means for pivoting the barrel to said member for swinging movement along the line of'flight of the aircraft, to

afford a lead for each position to which the barrel may have been rotated, and means for rotating said member.

7. A device for pointing agun at an aircraft in flight,-constructed.as set forthln claim 6, and wherein the last-specified means comprises a motor supportedfrom the carrier, anda driving 7 connection betweenthe motorand said member.

8. A device for pointing a gun atan aircraft in flight, constructed as set forth in claim 6, in combination with mechanism for swinging the barrel along said line of flight of theaircraft, said mechanism comprising a motor supported from the carrier and having a shaft, a pinion contudinal axis of the barrel to a point closely adja- 10 cent to the perimeter of the barrel, a carrier mounted for horizontal and for vertical swinging movements, a member mounting the barrel on the carrier for rotation in a plane transverse to the longitudinal axis of the barrel, to align the longer transverse dimension of the group with the path of flight of the aircraft, and means for rotating the barrel about its longitudinal axis.

JOHN ALLEN VEIT. 

